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A Control Moment Gyro (CMG) Based Attitude Control System (ACS) For Agile Small Satellites

Lappas, Vaios J (2002) A Control Moment Gyro (CMG) Based Attitude Control System (ACS) For Agile Small Satellites Doctoral thesis, University of Surrey.

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Item Type:Thesis (Doctoral)
Additional Information:Thesis submitted for the degree of Doctor of Philosophy, University of Surrey. Copyright remains with the author.
Divisions:Theses
ID Code:896
Deposited By:Mr Adam Field
Deposited On:27 May 2010 15:27
Last Modified:03 Sep 2010 16:13

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